Saturn MS-II-4(S)B

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Saturn MS-II-4(S)B

Part of Saturn II

LOx/LH2 propellant rocket stage. Standard S-II but with structural strength increased from 86% to 502% depending on station, resulting in 8.6% increase in empty weight.

Status: Study 1968. Thrust: 5,169.00 kN (1,162,037 lbf). Gross mass: 494,100 kg (1,089,300 lb). Unfuelled mass: 42,300 kg (93,200 lb). Specific impulse: 421 s. Specific impulse sea level: 200 s. Burn time: 355 s. Height: 24.84 m (81.49 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 5.

Country: USA. Engines: J-2. Launch Vehicles: Saturn MLV-V-4(S), Saturn V-23(L), Saturn V-24(L), Saturn V-25(S)B, Saturn V-4X(U), Saturn V-25(S)U. Propellants: Lox/LH2.

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